Patents by Inventor Robert T. Kendall, Jr.

Robert T. Kendall, Jr. has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 5630296
    Abstract: Temporary emergency structures comprising inflatable frameworks formed of ultra-high temperature resistant fabric tubing which may insulate the protected person or equipment from the ground and which serves to support a cover formed of ultra-high temperature resistant fabric cloth.
    Type: Grant
    Filed: August 25, 1994
    Date of Patent: May 20, 1997
    Inventor: Robert T. Kendall, Jr.
  • Patent number: 5297761
    Abstract: An improved cockpit area for manned atmospheric or space vehicles includes a generally spherical, multi-axis G-compensating cockpit capsule which houses the crewmen, together with the appropriate operational and navigational instruments and the mechanisms necessary for controlling the vehicle and which is rotatably mounted in the vehicle and is controllable by the crewman to permit the crewman direct visual observation throughout virtually a full circle about the vehicle, without altering the course of the vehicle, together with a device for automatically rotating the capsule to minimize the effect of high G-forces on the crewmen, and an emergency mechanism for ejecting the capsule, with the crewmen therein, and for protecting the crewmen during and after descent and landing of the capsule.
    Type: Grant
    Filed: June 15, 1992
    Date of Patent: March 29, 1994
    Inventors: Robert T. Kendall, Jr., Robert T. Kendall, Sr.
  • Patent number: 4832288
    Abstract: A recovery system for decelerating/stabilizing and protecting space vehicles, boosters, astronauts, equipment and like payloads, including a paracanopy defined by a frusto-conical flexible uninflated skin forming a decelerator/stabilizer surface having a small inflated torus at it leading end and a larger trailing torus at its trailing end with an inflated annular protective sheath therebetween protecting the payload housed therein, duct means between the toruses and the annular sheath for forming a fluidically rigidified frame, and the fluidically rigidified frame maintaining the flexible skin in taut though uninflated condition during entry and recovery, The paracanopy further can include an inflated buoyant section for recovery at sea, and depending upon the payload to be recovered, the paracanopy can be deployed as a single structure from one end of the payload or from opposite ends of the payload as two separate cooperative structures.
    Type: Grant
    Filed: July 23, 1987
    Date of Patent: May 23, 1989
    Assignee: Aerospace Recovery System, Inc.
    Inventors: Robert T. Kendall, Robert T. Kendall, Jr.